JP4719797B2 - Internal combustion engine operation method - Google Patents

Internal combustion engine operation method Download PDF

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JP4719797B2
JP4719797B2 JP2008520671A JP2008520671A JP4719797B2 JP 4719797 B2 JP4719797 B2 JP 4719797B2 JP 2008520671 A JP2008520671 A JP 2008520671A JP 2008520671 A JP2008520671 A JP 2008520671A JP 4719797 B2 JP4719797 B2 JP 4719797B2
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fuel
ignition
internal combustion
combustion engine
mixture
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JP2009500560A (en
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ベラン,ロベルト
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AVL List GmbH
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B43/00Engines characterised by operating on gaseous fuels; Plants including such engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B19/00Engines characterised by precombustion chambers
    • F02B19/10Engines characterised by precombustion chambers with fuel introduced partly into pre-combustion chamber, and partly into cylinder
    • F02B19/1019Engines characterised by precombustion chambers with fuel introduced partly into pre-combustion chamber, and partly into cylinder with only one pre-combustion chamber
    • F02B19/1023Engines characterised by precombustion chambers with fuel introduced partly into pre-combustion chamber, and partly into cylinder with only one pre-combustion chamber pre-combustion chamber and cylinder being fed with fuel-air mixture(s)
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D19/00Controlling engines characterised by their use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures
    • F02D19/06Controlling engines characterised by their use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures peculiar to engines working with pluralities of fuels, e.g. alternatively with light and heavy fuel oil, other than engines indifferent to the fuel consumed
    • F02D19/0602Control of components of the fuel supply system
    • F02D19/0607Control of components of the fuel supply system to adjust the fuel mass or volume flow
    • F02D19/061Control of components of the fuel supply system to adjust the fuel mass or volume flow by controlling fuel injectors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D19/00Controlling engines characterised by their use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures
    • F02D19/06Controlling engines characterised by their use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures peculiar to engines working with pluralities of fuels, e.g. alternatively with light and heavy fuel oil, other than engines indifferent to the fuel consumed
    • F02D19/08Controlling engines characterised by their use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures peculiar to engines working with pluralities of fuels, e.g. alternatively with light and heavy fuel oil, other than engines indifferent to the fuel consumed simultaneously using pluralities of fuels
    • F02D19/10Controlling engines characterised by their use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures peculiar to engines working with pluralities of fuels, e.g. alternatively with light and heavy fuel oil, other than engines indifferent to the fuel consumed simultaneously using pluralities of fuels peculiar to compression-ignition engines in which the main fuel is gaseous
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/0025Controlling engines characterised by use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures
    • F02D41/0027Controlling engines characterised by use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures the fuel being gaseous
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/30Controlling fuel injection
    • F02D41/38Controlling fuel injection of the high pressure type
    • F02D41/40Controlling fuel injection of the high pressure type with means for controlling injection timing or duration
    • F02D41/402Multiple injections
    • F02D41/405Multiple injections with post injections
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/30Use of alternative fuels, e.g. biofuels
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/40Engine management systems

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Oil, Petroleum & Natural Gas (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)

Description

本発明は、気体燃料で駆動される内燃機関を運転させるための方法であって、少なくとも1つのエンジン運転域において、主燃焼室に供給された燃料ガスと空気との混合気の燃焼が予燃焼室内の着火性燃料と空気との混合気の着火によって導かれ、その際、前記予燃焼室内において圧縮行程終了付近で液体燃料の自己着火によって燃焼する燃料と空気との混合気が生じるように構成されたものに関する。   The present invention is a method for operating an internal combustion engine driven by gaseous fuel, wherein combustion of a mixture of fuel gas and air supplied to a main combustion chamber is pre-combusted in at least one engine operating region. It is guided by ignition of a mixture of ignitable fuel and air in the room, and at that time, a mixture of fuel and air combusted by self-ignition of liquid fuel is generated in the pre-combustion chamber near the end of the compression stroke. Related to what was done.

少なくとも1つのエンジン運転域において、主燃焼室に供給された燃料ガスと空気との混合気の燃焼が予燃焼室における着火性燃料と空気との混合気の着火によって導かれる、気体燃料で駆動される内燃機関運転方法が知られている(例えば,特許文献1参照)。予燃焼室において燃料と空気との均質な混合気が発生させられ、予燃焼室内に生じたこの燃料と空気との均質な混合気は圧縮行程終了付近で自己着火プロセスによって自然かつ均質に燃焼する。これによって、エミッションをできるだけ低く保つと共に、高い効率を達成することが可能である。   In at least one engine operating region, the combustion of the mixture of fuel gas and air supplied to the main combustion chamber is driven by gaseous fuel guided by the ignition of the mixture of ignitable fuel and air in the precombustion chamber An internal combustion engine operating method is known (see, for example, Patent Document 1). A homogeneous mixture of fuel and air is generated in the pre-combustion chamber, and this homogeneous mixture of fuel and air generated in the pre-combustion chamber is naturally and uniformly burned by the self-ignition process near the end of the compression stroke. . This makes it possible to keep emissions as low as possible and achieve high efficiency.

予燃焼室式燃焼方法は、特に、一定のシリンダ行程容積以上のリーンバーン(つまり、高い空気/燃料比)方式で運転されるガス機関に適用される。主燃焼室での直接の燃焼開始ではなく予燃焼室で燃焼開始が行われる利点は、高い空気/燃料比であっても低い着火エネルギーでも十分にシリンダチャージ全体の効果的にもかかわらず有害物質排出の少ない燃焼が保証されることである。   The pre-combustion chamber combustion method is particularly applicable to gas engines that are operated in a lean burn (ie, high air / fuel ratio) mode with a certain cylinder stroke volume or higher. The advantage of starting combustion in the pre-combustion chamber rather than starting combustion directly in the main combustion chamber is that the high air / fuel ratio or low ignition energy is sufficient for toxic substances despite the effectiveness of the entire cylinder charge This means that combustion with low emissions is guaranteed.

燃料ガスと空気との混合気は圧縮行程の間に主燃焼室から予燃焼室に流入し、その結果、予燃焼室内に燃焼性混合気が生ずる。この燃料ガスと空気との混合気の着火のため、従来、電気点火システムまたはパイロット噴射方式が利用されている。電気火花点火の場合には、燃焼開始場所において主燃焼室に比較して著しく濃厚で、着火し易い混合気を得るために、さらになお多くの純粋な燃料ガスまたは燃料ガスと空気との混合気が予燃焼室内に供給される。電気点火システムの場合には、点火プラグの電極間の点火火花のフラッシオーバによって燃焼が開始されるが、他方、パイロット噴射方式の場合には、少量の液体燃料が高圧で予燃焼室内に噴射される。これは十分に高い圧縮温度時に自己着火し、続いて燃料ガスと空気との混合気の燃焼を導く。   A mixture of fuel gas and air flows from the main combustion chamber into the precombustion chamber during the compression stroke, resulting in a combustible mixture in the precombustion chamber. Conventionally, an electric ignition system or a pilot injection system has been used to ignite the mixture of fuel gas and air. In the case of electric spark ignition, in order to obtain a mixture that is significantly richer and easier to ignite compared to the main combustion chamber at the start of combustion, still more pure fuel gas or a mixture of fuel gas and air is required. Is supplied into the pre-combustion chamber. In the case of an electric ignition system, combustion is started by a flashover of an ignition spark between the electrodes of the spark plug. On the other hand, in the case of the pilot injection method, a small amount of liquid fuel is injected into the precombustion chamber at a high pressure. The This is self-igniting at a sufficiently high compression temperature and subsequently leads to the combustion of a mixture of fuel gas and air.

主燃焼室内の燃料ガスと空気との混合気は予燃焼室から流れ込む火炎によって着火される。   The mixture of fuel gas and air in the main combustion chamber is ignited by a flame flowing from the precombustion chamber.

予燃焼室内に高圧縮気体燃料が吹き込まれてそこで着火させられる、混合気圧縮過給式ガス機関の運転を最適化するための方法が公知である(例えば特許文献2参照)。この場合、吹き込みは約250乃至300barの圧力下で行われる。これには比較的高コストの吹き込みシステムが必要である。燃料の高圧縮化は付加的な仕事の発生と、それゆえの付加的な効率低下をもたらす。   A method for optimizing the operation of an air-fuel mixture compression supercharged gas engine in which a highly compressed gaseous fuel is blown into a precombustion chamber and ignited there is known (see, for example, Patent Document 2). In this case, the blowing is performed under a pressure of about 250 to 300 bar. This requires a relatively expensive blowing system. Higher fuel compression results in additional work and hence additional efficiency reduction.

電気点火方式およびパイロット噴射方式の短所は、予燃焼室内に窒素酸化物が多量に発生すると共に、場合により、これらの有害物質の排出量を相対的に高めるかなりの量の粒子も発生することである。他方、これらのエミッションに関する最適化技術もまた、予燃焼室から溢れ出る火炎のエネルギーが低く、したがって、主燃焼室内の燃焼が緩慢で、効率が悪化するという短所を有している。特に電気点火式の技術は点火プラグの寿命が限られているというさらに重大な短所を有している。   The disadvantages of the electric ignition and pilot injection systems are that a large amount of nitrogen oxides are generated in the pre-combustion chamber, and in some cases, a considerable amount of particles that relatively increase the emission of these harmful substances is also generated. is there. On the other hand, these emission optimization techniques also have the disadvantage that the energy of the flame overflowing from the pre-combustion chamber is low, and therefore the combustion in the main combustion chamber is slow and the efficiency deteriorates. In particular, the electric ignition type technology has a further serious disadvantage that the life of the spark plug is limited.

オーストリア登録実用新案第006290号明細書Austrian registered utility model No.006290 ドイツ出願公開第4419429号明細書German Application No. 4419429

本発明の目的は、気体燃料で駆動される内燃機関を運転させるための方法であって、効率のさらなる向上とエミッションの低減を達成することができる内燃機関運転方法を提供することである。   An object of the present invention is to provide a method for operating an internal combustion engine driven by gaseous fuel, which can achieve further improvement in efficiency and reduction in emissions.

上記目的を達成するため、本発明による内燃機関運転方法では、少なくとも1つのエンジン運転域において、主燃焼室に供給された燃料ガスと空気との混合気の燃焼が予燃焼室内の着火性燃料と空気との混合気の着火によって導かれ、その際、前記予燃焼室内において圧縮行程終了付近で液体燃料の自己着火によって燃焼する燃料と空気との混合気が生じるように構成され、1つの作動サイクルの間に液体燃料が前記予燃焼室内に複数回噴射される。   In order to achieve the above object, in the internal combustion engine operating method according to the present invention, in at least one engine operating region, combustion of a mixture of fuel gas and air supplied to the main combustion chamber is performed with ignitable fuel in the precombustion chamber. A mixture of fuel and air that is guided by the ignition of a mixture with air and burns by the self-ignition of liquid fuel near the end of the compression stroke in the pre-combustion chamber; In the meantime, the liquid fuel is injected into the pre-combustion chamber a plurality of times.

その際、好ましくは、少なくとも初回の噴射は、着火上死点前180°と本来の着火時点の直前までの間の領域内で行われ、好ましくは少なくとも第2回の噴射は圧縮行程の後半に、好ましくは上死点前30°と上死点までの間の領域内で行われる。この場合、前記初回噴射の燃料量は前記第2回の噴射燃料量よりも多くてもよい。 At this time, it is preferable that at least the first injection is performed in a region between 180 ° before ignition top dead center and immediately before the original ignition time point, and preferably at least the second injection is performed in the latter half of the compression stroke. Preferably, it is carried out in the region between 30 ° before top dead center and top dead center. In this case, the fuel amount of the first injection may be larger than the second injected fuel amount.

前記初回の噴射が圧縮行程の早期相で行われることにより、前記予燃焼室内において燃料と空気との混合気の広範な均質化が達成される。着火上死点の領域における前記第2回の燃料噴射は本来の着火に使用され、その際、前記着火には非常に少量の燃料しか必要でない。   By performing the initial injection in the early phase of the compression stroke, wide homogenization of the fuel / air mixture in the pre-combustion chamber is achieved. The second fuel injection in the ignition top dead center region is used for the original ignition, in which case only a very small amount of fuel is required for the ignition.

複数回噴射と前記少量の2回目の噴射とによって、点火時点には予燃焼室内に不均質な混合気成分は僅かに存在するにすぎず、そのため、前記予燃焼室内の燃料は非常に急速かつ有害物質低発生量の下で燃焼することができる。これは一方で、粒子およびNOxエミッションに有利に作用すると共に、他方で、前記予燃焼室内のより多くのエネルギーが主燃焼室におけるより急速な燃焼に利用される結果をもたらす。結果として、より高い平均圧力が達成されることにより、より高い効率を達成することができる。   Due to the multiple injections and the small amount of the second injection, there is only a slight heterogeneous mixture component in the precombustion chamber at the time of ignition, so that the fuel in the precombustion chamber is very rapid and It can be burned under a low generation amount of harmful substances. This, on the one hand, favors particle and NOx emissions, and on the other hand results in more energy being utilized in the main combustion chamber for faster combustion. As a result, higher efficiency can be achieved by achieving a higher average pressure.

以下に本発明を、図面を参照して詳細に説明する。   Hereinafter, the present invention will be described in detail with reference to the drawings.

図1は往復ピストン2を備えた、気体燃料で駆動される内燃機関のシリンダ1を概略的に示している。燃料ガスと空気との混合気は吸気路3を経て吸気弁4の開放時に主燃焼室5内に流入し、その後、圧縮行程中に予燃焼室6内に押し込まれる。予燃焼室6内には噴射装置7によって燃料が複数回噴射され、その際、初回の燃料噴射は、着火上死点前180°のクランク角から本来の着火時点の直前までの間の領域内で行われる。この早期燃料噴射によって、予燃焼室6内に燃料と空気とのほぼ均質な混合気が形成される。本来の着火は着火上死点の領域での噴射装置7による2回目の燃料噴射によって実現する。その際、2回目の燃料噴射量は非常に僅かである。これにより、2回目の噴射に起因するエミッションをできるだけ低く抑えることができる。ただし、燃焼室温度が非常に高い場合には、早すぎ着火を回避するため、初回の燃料噴射量を2回目の噴射に比較して僅かに抑える程度のものとすることも好適である。
FIG. 1 schematically shows a cylinder 1 of an internal combustion engine with a reciprocating piston 2 driven by gaseous fuel. The mixture of fuel gas and air flows into the main combustion chamber 5 through the intake passage 3 when the intake valve 4 is opened, and is then pushed into the precombustion chamber 6 during the compression stroke. The fuel is injected into the pre-combustion chamber 6 a plurality of times by the injection device 7. At this time, the first fuel injection is performed in a region from a crank angle of 180 ° before ignition top dead center to immediately before the original ignition time. Done in By this early fuel injection, a substantially homogeneous mixture of fuel and air is formed in the precombustion chamber 6. The original ignition is realized by the second fuel injection by the injection device 7 in the ignition top dead center region. At that time, the second fuel injection amount is very small. Thereby, the emission resulting from the second injection can be kept as low as possible. However, when the combustion chamber temperature is very high, in order to avoid ignition too early, it is also preferable that the initial fuel injection amount be suppressed slightly compared to the second injection.

予燃焼室6は、1つのまたは複数の孔8を介して主燃焼室5と流通している。2回目の燃料噴射によって、予燃焼室6内にある燃料と空気との均質な混合気は圧縮行程の終了付近で、つまりピストン2が着火上死点に達する直前に着火させられ、それにより、予燃焼室6内の混合気全体が燃焼する。この自己着火プロセスを確実に開始させ得るように、加熱装置9又は断熱あるいはその両方による予燃焼室6の壁面の加熱が行なわれてもよい。   The precombustion chamber 6 is in communication with the main combustion chamber 5 via one or a plurality of holes 8. By the second fuel injection, the homogeneous mixture of fuel and air in the pre-combustion chamber 6 is ignited near the end of the compression stroke, that is, immediately before the piston 2 reaches the top dead center of ignition, The entire air-fuel mixture in the precombustion chamber 6 is combusted. The wall surface of the precombustion chamber 6 may be heated by the heating device 9 and / or heat insulation so that the self-ignition process can be started reliably.

着火補助として、始動時には、場合により、予燃焼室6内または主燃焼室5内に取り付けられた点火プラグおよびグロープラグ10を使用することができる。   As ignition assistance, an ignition plug and a glow plug 10 attached in the precombustion chamber 6 or the main combustion chamber 5 can be used at the time of start-up.

予燃焼室6内における特に急速な燃焼は、高い圧力上昇と、その後に主燃焼室5内の燃料ガスと空気との混合気を着火させる極めて高いインパルスを有した高エネルギーの火炎とをもたらす。主燃焼室5内の燃焼挙動は予燃焼室6内の燃焼と同様に火炎面の動きに左右される。   Particularly rapid combustion in the precombustion chamber 6 results in a high pressure rise and a high energy flame with a very high impulse that subsequently ignites the mixture of fuel gas and air in the main combustion chamber 5. The combustion behavior in the main combustion chamber 5 depends on the movement of the flame surface as in the combustion in the precombustion chamber 6.

上述した方法は、特にNOxおよび粒子の最小限のエミッションならびに非常に高い効率を実現することを特徴としている。こうした低エミッションは、不均質なディーゼル分が減少させられて、極めて僅かのNOxと粒子しか形成されず、主燃焼室5内でもこれらの有害物質が十分に高い空燃比によって同じく低く抑えられることによる。主燃焼室5内の高空燃比にもかかわらず、予燃焼室6から主燃焼室5内に流れ込む高エネルギーの火炎によって、高効率の急速な燃焼が保証される。
これらの結果、最高効率と同時に最小限のNOxおよび粒子エミッションの実現が可能になる。
The method described above is particularly characterized in that it achieves a minimum emission of NOx and particles and a very high efficiency. This low emission is due to the reduced heterogeneous diesel content, resulting in very little NOx and particle formation, and even in the main combustion chamber 5 these harmful substances are also kept low by a sufficiently high air / fuel ratio. . Despite the high air-fuel ratio in the main combustion chamber 5, high-efficiency rapid combustion is ensured by the high-energy flame flowing from the pre-combustion chamber 6 into the main combustion chamber 5.
As a result, it is possible to achieve a minimum NOx and particle emission as well as a maximum efficiency.

本発明による方法によって運転される、気体燃料で駆動される内燃機関のシリンダ1を概略的に示す模式図Schematic diagram schematically showing a cylinder 1 of an internal combustion engine driven by gaseous fuel, operated by the method according to the invention.

Claims (5)

気体燃料で駆動される内燃機関を運転させるための方法であって、
少なくとも1つのエンジン運転域において、主燃焼室(5)に供給された燃料ガスと空気との混合気の燃焼が予燃焼室(6)内の着火性燃料と空気との混合気の着火によって導かれ、その際、前記予燃焼室内において圧縮行程終了付近で液体燃料の自己着火によって燃焼する燃料と空気との混合気が生じるように構成され、1つの作動サイクルの間に液体燃料が前記予燃焼室(6)内に複数回噴射されることを特徴とする内燃機関運転方法。
A method for operating an internal combustion engine driven by gaseous fuel comprising:
In at least one engine operating region, the combustion of the mixture of fuel gas and air supplied to the main combustion chamber (5) is guided by the ignition of the mixture of ignitable fuel and air in the precombustion chamber (6). In this case, a mixture of fuel and air combusted by self-ignition of the liquid fuel is generated in the precombustion chamber in the vicinity of the end of the compression stroke, and the liquid fuel is combusted during one operation cycle. An internal combustion engine operating method, characterized in that the fuel is injected a plurality of times into the chamber (6).
少なくとも初回の噴射は、着火上死点前180°のクランク角から本来の着火時点の直前までの間の領域で行われることを特徴とする請求項1に記載の内燃機関運転方法。2. The internal combustion engine operating method according to claim 1, wherein at least the first injection is performed in a region between a crank angle of 180 [deg.] Before ignition top dead center and immediately before the original ignition time. 少なくとも2回目の噴射は圧縮行程の後半に、好ましくは上死点前30°と上死点までの間の領域内で行われることを特徴とする請求項1又は2に記載の内燃機関運転方法。  The internal combustion engine operating method according to claim 1 or 2, wherein at least the second injection is performed in the latter half of the compression stroke, preferably in a region between 30 ° before top dead center and top dead center. . 初回噴射の燃料量は2回目の噴射燃料量よりも多いことを特徴とする請求項3に記載の内燃機関運転方法。  4. The internal combustion engine operating method according to claim 3, wherein the amount of fuel for the first injection is larger than the amount of fuel injected for the second time. 初回の噴射後に前記予燃焼室(6)内に燃料と空気との均質な混合気が生ずることを特徴とする請求項1から4のいずれか一項に記載の内燃機関運転方法。  The method for operating an internal combustion engine according to any one of claims 1 to 4, wherein a homogeneous mixture of fuel and air is produced in the precombustion chamber (6) after the first injection.
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